View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 36089U 09061B 24281.94690610 .00002322 00000-0 57036-3 0 9997
2 36089 98.3740 247.2404 0080429 129.7251 231.1069 14.51341229788605
Epoch (UTC): | 07 October 2024 22:43:32 |
Eccentricity: | 0.0080429 |
inclination: | 98.3740° |
perigee height: | 664 km |
apogee height: | 778 km |
right ascension of ascending node: | 247.2404° |
argument of perigee: | 129.7251° |
revolutions per day: | 14.51341229 |
mean anomaly at epoch: | 231.1069° |
orbit number at epoch: | 78860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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